A PC Based Conceptual Design Package for Composite Bolted Joints

975534

10/01/1997

Event
World Aviation Congress & Exposition
Authors Abstract
Content
A user friendly Windows™ based software package is developed for analysis and design of single lap and double lap bolted joints. The bolted joint design software is based on the computer codes developed by the Northrop Corporation under a contract from the Wright Laboratory, Wright-Patterson Air Force Base, OH. Due to the low analysis time requirements, the software package is an efficient tool for use in design and optimization cycle of bolted joints involving composite materials. This work is conducted as part of a larger effort currently underway at the AdTech Systems Research, Inc. to establish a baseline to extend the joint design methodology for generalized composite systems including life prediction, thermal effects and dissimilar materials.
Meta TagsDetails
DOI
https://doi.org/10.4271/975534
Pages
12
Citation
Rastogi, N., Kochetkov, V., Deepak, B., and Nagar, A., "A PC Based Conceptual Design Package for Composite Bolted Joints," SAE Technical Paper 975534, 1997, https://doi.org/10.4271/975534.
Additional Details
Publisher
Published
Oct 1, 1997
Product Code
975534
Content Type
Technical Paper
Language
English